The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida.
Specifications
- Thrust
- 1,704 kN
- Height
- 33 m
- Diameter
- 3.05 m
- Launch mass
- —
- Stages
- 2
- Launch cost
- —
- LEO capacity
- —
- GTO capacity
- 1,800 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
4
Launches with a definitive outcome
Success rate
50%
2 of 4
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Atlas Centaur | Surveyor-SD 1 — Failure
- Atlas Centaur | Surveyor Mass Model — Success
- Atlas Centaur | AC-3 Instrumentation Ring — Failure
- Atlas Centaur | AC-2 Instrumentation Ring — Success